| タイトル | SSME/side loads analysis for flight configuration, revision A |
| 本文（外部サイト） | http://hdl.handle.net/2060/19750002092 |
| 著者（英） | Holland, W. |
| 著者所属（英） | NASA Marshall Space Flight Center |
| 発行日 | 1974-09-01 |
| 言語 | eng |
| 内容記述 | This document describes the dynamic loads analysis accomplished for the Space Shuttle Main Engine (SSME) considering the side load excitation associated with transient flow separation on the engine bell during ground ignition. The results contained herein pertain only to the flight configuration. A Monte Carlo procedure was employed to select the input variables describing the side load excitation and the loads were statistically combined. This revision includes an active thrust vector control system representation and updated orbiter thrust structure stiffness characteristics. No future revisions are planned but may be necessary as system definition and input parameters change. |
| NASA分類 | SPACECRAFT PROPULSION AND POWER |
| レポートNO | 75N10164
NASA-TM-X-64841 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/192384 |
